787 MEMORY ITEMS Flashcards

1
Q

ABORTED ENGINE START L,R

A

1) FUEL CONTROL SWITCH (AFFECTED SIDE)….. CUTOFF

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2
Q

ENG AUTOSTART L,R

A

FUEL CONTROL SWITCH (affected side)……. CONFIRM……CUTOFF

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3
Q

DUAL ENG FAIL/STALL

A

FUEL CONTROL SWITCHES (BOTH) ….. CUTOFF THEN RUN

RAM AIR TURBINE SWITCH …. PUSH AND HOLD FOR 1 SEC

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4
Q

ENG LIMIT EXCEEDED, SURGE, OR STALL L,R

A

1) AT ARM SWITCH … CONFIRM AND OFF
2) THRUST LEVER … CONFIRM AND RETARD UNTIL EXCEED MESSAGE IS BLANK
OR THRUST LEVER IDLE

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5
Q

SMOKE OR FIRE FROM LITHIUM BATTERY

A

1) TRANSFER CONTROL IF NEEDED TO CREW OPPOSITE TO FIRE
2) PA BACKUP TO THE FLIGHT DECK x2

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6
Q

SMOKE FIRE FUMES

A

1) OXYGEN AND SMOKE MASK….ON 100%
2) CREW AND CABIN COMMS…. ESTABLISH

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7
Q

STABILIZER

A

1) STAB CUTOUT SWITCHES (Both)… CUTOUT
2) DO NOT EXCEED CURRENT SPEED

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8
Q

AIRSPEED UNRELIABLE

A

1) AUTOPILOT…. DISCONNECT
2) AT ARM SWITCHES (Both)…. OFF
3) F/D SWITCHES (Both)…..OFF
FLAPS EXTENDED - 10 degrees 85%N1
FLAPS RETRACTED - 4 degrees 70%N1

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9
Q

OCEANIC DIVERSION - ALL ENGINE

A

1) INITIATE APPLICABLE DRILLS AND TIME CRITICAL CHECKLISTS
2) DECLARE EMERGENCY AND REQUEST CLEARANCE

IF CLEARANCE OBTAINED - PROCEED PER CLEARANCE

IF CLEARANCE UNAVAILABLE
TURN ATLEAST AND OFFSET
OCA 30 RIGHT OR LEFT 5NM
CHINA 30 RIGHT 5NM
RUSSIA 30 RIGHT 16.2NM

WHEN ESTABLISHED, +- 500FT

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10
Q

OCEANIC DIVERSION - ENGINE OUT

A

1) INITIATE APPLICABLE DRILLS AND TIME CRITICAL CHECKLISTS
2) DECLARE EMERGENCY AND REQUEST CLEARANCE

IF CLEARANCE OBTAINED - PROCEED PER CLEARANCE

IF CLEARANCE UNAVAILABLE
TURN ATLEAST AND OFFSET
OCA 30 RIGHT OR LEFT 5NM
CHINA 30 RIGHT 5NM
RUSSIA 30 RIGHT 16.2NM

WHEN ESTABLISHED, DESCEND BELOW FL290 AND MAINTAIN +/- 500FT

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11
Q

FIRE ON GROUND

A

FIRE ON GROUND CHECKLIST

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12
Q

PASSENGER EVACUATION

A

PASSENGER EVACUATION CHECKLIST

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13
Q

MAX LANDING WEIGHTS 787-8/787-9

A

787-8 - 172 365
787-9 - 192 776

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14
Q

WINDSHEAR MANUAL FLIGHT

A

1) Call “WINDSHEAR TOGA” and disconnect
autopilot.
2) Push either TO/GA switch.
3) Aggressively apply maximum* thrust.
4) Disconnect autothrottle(s).
5) Simultaneously roll wings level and rotate toward an
initial pitch attitude of 15°.
6) Retract speedbrakes.
7) Follow flight director TO/GA guidance (if available)

Do not change gear or flap configuration.
Maintain wings level to maximize climb gradient. Unless turn required
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed

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15
Q

WINDSHEAR AUTOMATIC FLIGHT

A

Call “WINDSHEAR TOGA”
Push either TO/GA switch.*
Verify TO/GA mode annunciation.
Verify thrust advances to GA* power.
Retract speedbrakes.
Monitor system performance
**

Do not change gear or flap configuration.
Maintain wings level to maximize climb gradient. Unless turn required
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed

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16
Q

DRIFTDOWN

A

PF - Request ENG OUT to be selected on the FMC PM - SELECT ENG OUT ON FMC CRZ PAGE
ACT CRZ page

ENSURE VNAV ENGAGED
Set EO ALT IN ALT WINDOW
CALL EXECUTE PM - Execute FMC, turn on all exterior lights, advise ATC

Initiate Turn
Call Checklist engine failure PM complete the checklist

At altitude capture confirm ENG OUT CRZ page
is displayed. Maintain MCT and drift down
altitude until the EO speed is established.
Proceed to land at the nearest suitable airport